function [p,f,g,h,k,L] = lowThrustCoe2Mee(a,ecc,inc,Ome,ome,nu)

p = a.*(1-ecc.^2);
f = ecc.*cos(ome+Ome);
g = ecc.*sin(ome+Ome);
h = tan(inc/2).*cos(Ome);
k = tan(inc/2).*sin(Ome);
L = Ome+ome+nu;

end
